Method and system for using a MEMS structure as a timing source

ABSTRACT

A system and method is disclosed that provides a technique for generating an accurate time base for MEMS sensors and actuators which has a vibrating MEMS structure. The accurate clock is generated from the MEMS oscillations and converted to the usable range by means of a frequency translation circuit.

CROSS-REFERENCE TO RELATED APPLICATION

Under 35 U.S.C. §120 the present application is a continuation of U.S.patent application Ser. No. 12/418,547, filed Apr. 3, 2009, entitled“METHOD AND SYSTEM FOR USING A MEMS STRUCTURE AS A TIMING SOURCE,” whichis incorporated herein by reference.

FIELD OF THE INVENTION

The present invention relates generally to MEMS devices and morespecifically to MEMS devices with a vibrating MEMS structure, whereinthe primary function of the MEMS structure is not to provide an accurateclock.

BACKGROUND OF THE INVENTION

MEMS devices with integrated IC electronics are being used in manyconsumer applications. For example, MEMS accelerometers are used in airbag deployment, MEMS gyros provide hand jitter information for imagestabilization in digital cameras, MEMS microphones are replacingconventional electret microphones in cell phones, vibrating mirrorsenable ultra small projectors for consumer applications. In the earlierMEMS devices, the sensor output was usually provided to the outsideworld by analog signals. In recent years, consumer applications startedto require additional features from the MEMS devices. These additionalfeatures include providing digital outputs, digital filtering, andinterrupt generation upon detecting certain ranges of sensor data. Evenfurther, many inertial sensors include algorithms or features fordetection of complex movements and gestures. These additional featuresare implemented using digital circuits and the accuracy of thesecircuits is determined by the accuracy of the clock signal. Especially,for navigation applications, accuracy of the timing is crucial.Applications such as GPS assist and dead reckoning rely on integrationof motion sensor output to determine orientation and position. Theaccuracy of the integration time steps is determined by the accuracy ofthe clock.

There are two common types of oscillator circuits: relaxationoscillators and harmonic oscillators. In relaxation oscillators, anenergy storing device (capacitor or inductor) is charged and dischargedby a non-linear circuit component. This cycle is repeated indefinitelycreating a periodic signal which is usually a saw tooth wave. FIG. 1shows an example of a relaxation oscillator circuit. In this circuit,the capacitor C_(C) (103) is charged through the resistor R_(C) (102).

The voltage at node A increases as the capacitor charge increases. TheSchmitt trigger 101 output stays low if the input is below certainthreshold value, LH, or goes to high if the input exceeds anotherthreshold value, HI. The capacitor voltage or the voltage at node A inthis circuit controls the output of the buffer. When the voltage exceedsthe high threshold voltage of the Schmitt trigger buffer 101, the bufferoutput becomes logic high closing the switch 104. The capacitor isdischarged through the switch 104. When the capacitor voltage dropsbelow the low threshold, Schmitt trigger buffer 101 output goes back tologic low opening the switch 104. At this point, the resistor startscharging the capacitor again. This cycle repeats continuously creating asquare wave at the buffer output. The oscillation frequency of thecircuit is determined by the R_(C)C_(C) time constant. Small changes inthe R or C values directly affect the oscillation frequency.

Harmonic oscillators on the other hand generate a sinusoidal signal.FIG. 2 shows such a circuit. The output of an amplifier 201 is fed tothe input of the amplifier through a filter 202 as shown in FIG. 2. Thephase shifter 203 ensures that the oscillations are sustained byadjusting the overall loop phase to zero. The quality factor of thefilter limits the stability of the frequency and the phase noise of theoscillator. For increased accuracy, mechanical elements such as quartzcrystals or MEMS structures with high Q are used as the frequencydetermining elements.

In many integrated MEMS devices, the clock signal is usually generatedby a relaxation oscillator due to its simplicity, small area requirementand low power consumption. However, the frequency of this circuit is afunction of the resistive and capacitive circuit components which maychange with process parameters or temperature. For example, typicallythe resistor values change 10% over 100 degree C., resulting 10%frequency shift over the specified temperature range. On the other hand,a crystal filter provides a very accurate clock signal but using thesefilters is prohibited by the cost and size requirements of the consumerapplications.

There is a need for generating an accurate timing base in MEMS deviceswithout using an external quartz crystal or another source. The presentinvention addresses such a need.

SUMMARY OF THE INVENTION

A method of providing an accurate clock source for electronics thatsupport a MEMS device which has a vibrating MEMS structure is described.The accurate clock is obtained from the oscillating MEMS itself withminimal additional cost. The MEMS oscillation frequency is used as thereference signal for a frequency translator circuit such as PLL, DLL orfrequency multiplier which generates the timing source for thesupporting electronics.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a diagram of a relaxation oscillator.

FIG. 2 is a diagram of a harmonic oscillator.

FIG. 3 is a diagram of an oscillating MEMS device.

FIG. 4 is a diagram of an oscillating MEMS device where the clock to thedigital support electronics is provided by an oscillator circuit thatuses circuit elements.

FIG. 5 is a diagram of a MEMS device where the clock to the supportelectronics is generated from the oscillatory micromechanical structure.

FIG. 6 is a diagram of a vibratory MEMS gyro where the clock signal forthe digital electronics is provided by the resonating mechanicalstructure.

FIG. 7 is a diagram of a phase locked loop circuit.

FIG. 8 is a diagram of a tri-axis MEMS gyroscope where the clock to thesupport electronics can be obtained from one of the axes.

FIG. 9 is a diagram of a technique where a MEMS sensor provides clockfor an external system.

DETAILED DESCRIPTION

The present invention relates generally to MEMS devices and morespecifically to MEMS devices with a vibrating MEMS element. Thefollowing description is presented to enable one of ordinary skill inthe art to make and use the invention and is provided in the context ofa patent application and its requirements. Various modifications to thepreferred embodiments and the generic principles and features describedherein will be readily apparent to those skilled in the art. Thus, thepresent invention is not intended to be limited to the embodimentsshown, but is to be accorded the widest scope consistent with theprinciples and features described herein.

A variety of MEMS devices uses vibrating micromechanical structures.Vibratory MEMS gyroscopes, resonant accelerometers and scanning MEMSmirrors are some examples of such devices. The resonant structure inthese devices provides a high Q as well as the oscillation frequency isvery stable over temperature. In general, a MEMS structure 301 is placedinto oscillatory state as shown in FIG. 3. In the most general form, theMEMS structure 301 has a sense system 303 and a drive system 302. Themotion of the micromechanical structure is detected by the sense system303. The sense system 303 can be capacitive, piezoresistive,piezoelectric or optical. The output of the sense system 303 isconverted into electrical signals by a circuit and amplified by anamplifier 304. The phase of the amplified signal is adjusted by thephase shifter 305 appropriately at the oscillating frequency. Theoverall loop phase should be zero to satisfy oscillation condition suchthat oscillations build up. Another condition that needs to be satisfiedfor oscillation is that the overall loop gain should be equal to orlarger than 1. The drive system 302 moves the MEMS structureproportional to the applied signal. The drive system 302 can becapacitive, piezoelectric, thermal or another actuation method that iscommon to MEMS systems. When the position signal is applied to the drivesystem with proper gain and phase as explained above, the MEMS systemstarts to vibrate at its resonant frequency.

FIG. 4 shows a typical MEMS device with a resonating micromechanicalstructure. In this device micromechanical structure 401 is oscillatingby the feedback loop that is part of the analog electronics 402. Theclock for the digital electronics 403 is provided by another oscillatorcircuit 404 that is composed of electrical components. As an examplethis MEMS device can be a vibratory gyroscope. In this case, the sensorsenses the Coriolis input and converts it to an electrical signal. TheMEMS device can also be an actuator as in the case of scanning mirrors.Scanning mirrors scan an optical beam reflecting off their surface.

FIG. 5 shows the general idea in accordance with the present invention.The MEMS device 501 can be sensor or actuator whose primary objective isnot to provide an accurate timing source. For example, vibratorygyroscopes have a resonating micromechanical structures but theirprimary function is to detect Coriolis force. The resonating MEMSstructure aside from actuating the proof masses also provide a verystable oscillation frequency. The output frequency after translated by afrequency translator 504 can be used to provide an accurate clock forthe support electronics.

FIG. 6 shows a schematic drawing of a vibratory MEMS gyroscopestructure. The MEMS gyroscope structure is composed three subsystems:drive system 601, sense system 602 and Coriolis sense system 603. Thedrive and sense system is put into oscillation through a loop thatcontains automatic gain control (AGC) 607, phase shifter 606, andamplifiers 604 and 610. The MEMS motion is detected by the sense system602 and sense electronics 604. The amplitude of the MEMS oscillation iscontrolled by the AGC circuit 607. The phase shifter 606 adjusts thephase in the loop such that oscillation condition is met. Once the MEMSgyroscope structure is set into oscillation, the oscillation is verystable and the frequency shifts only fractional amounts with thetemperatures. The angular rotation velocity is sensed by the Coriolissense system 603 and the supporting electronics. In this system,Coriolis output is a sinusoidal signal whose output is determined by therotational velocity. Sense amplifier 611 detects the Coriolis signal.After demodulator 613, this signal is converted to the base band.Anti-aliasing filter (AAF) 614 removes the high order frequencycomponents on the Coriolis signal. The output of the AAF is an analograte signal which can be converted to a digital signal by the integratedelectronics. For this conversion an ADC 615 can be used. Digital lowpass filter 620 and motion processor 621 further process the gyrooutput. The digital blocks shown in the FIG. 6 require an accurate clockfor proper operation. This clock can be obtained from the oscillatorloop as shown through a frequency translator 622.

In most of the MEMS devices, a typical MEMS resonant frequency is from 5kHz to 50 kHz. Although this frequency is very stable, it is very low tobe used in most of the digital circuitry. It needs to be multiplied tobe in between 100 kHz to 1 GHz by using a frequency translator 622 asshown in FIG. 6.

One method of achieving the multiplication is to use a PLL circuit asshown in FIG. 7. The circuit is composed of a multiplier 704, loopfilter 702, voltage controlled oscillator (VCO) 701, and a divider 703.In this circuit, the reference signal which is generated by the MEMSoscillator is first divided by a divider 705 then it is multiplied bythe VCO 701 output. The multiplication generates a DC component and highfrequency components. The high frequency components are filtered out bythe low pass filter 702. The filter output drives the input of a voltagecontrolled oscillator. The frequency of the VCO is divided by aprogrammable divider 703. The output of the PLL then is a multipliedversion of the reference signal which is provided by the oscillatingMEMS. Other examples of frequency translators that could be utilized toperform this function include but are not limited to delay locked loops,frequency multipliers or the like.

FIG. 8 shows a block diagram of a tri-axis MEMS gyroscope. Each axis hasits own oscillator loop which has been shown in details in FIG. 7. Inthis device, the clock to the digital circuitry can be taken from one ofthe axes through the multiplexer 802. Frequency translator 804, convertsthe gyro oscillation frequency to the frequencies suitable for thedigital circuitry. This schema also enables synchronization of the gyroADCs i.e. each axis is sampled at the same instance.

FIG. 9 shows a system where the clock signal is provided on-board thedigital circuitry 905 from a MEMS device 901. The MEMS device 901 herecan be one of the vibratory MEMS sensors or actuators. The clockgenerated by this device can be used to drive the on board digitalcircuitry 905. Accordingly, the driven circuitry can be on the same die(System On Chip), circuitry on a separate die in a common package(System In Package), or circuitry in separate packages on one or moreprinted circuit boards.

Another circuit where an accurate clock is needed is a radiotransmitter. For this type of circuit the accuracy of the transmissionfrequency is important. This frequency can be generated from a vibratingMEMS device in accordance with an embodiment of the present invention.

In addition to generating the clock signal from the vibrating MEMSdevice, the temperature dependence of the clock can be further improvedby means of temperature compensation techniques. Such temperaturecompensation techniques are described, for example, in U.S. Pat. No.7,453,324, “Frequency and/or phase compensated microelectromechanicaloscillator,” assignee: Robert Bosch GmbH; U.S. Pat. No. 7,427,905,“Temperature controlled MEMS resonator and method for controllingresonator frequency,” assignee: Robert Bosch GmbH; U.S. Pat. No.7,362,197, “Temperature compensation for silicon MEMS resonator,”assignee: Robert Bosch GmbH; U.S. Pat. No. 7,224,236, “Frequency and/orphase compensated microelectromechanical oscillator,” assignee: RobertBosch GmbH; and U.S. Pat. No. 7,202,761, “Temperature compensation forsilicon MEMS resonator,” assignee: Robert Bosch GmbH.

Although the present invention has been described in accordance with theembodiments shown, one of ordinary skill in the art will readilyrecognize that there could be variations to the embodiments and thosevariations would be within the spirit and scope of the presentinvention. Accordingly, many modifications may be made by one ofordinary skill in the art without departing from the spirit and scope ofthe appended claims.

What is claimed is:
 1. A motion sensor comprising: a MEMS structure, wherein the MEMS structure oscillates at a resonant frequency and provides a sense signal responsive to a movement of the motion sensor; an electronic circuit coupled to the MEMS structure to provide a drive signal responsive to the oscillation of the MEMS structure at the resonant frequency and to detect the sense signal; a frequency translation circuit for receiving the drive signal, wherein the drive signal is translated to provide a clock signal; and a digital circuit coupled to the frequency translation circuit and the electronic circuit, wherein the clock signal is utilized to drive the digital circuit and the digital circuit provides a digital signal that is related to the movement of the motion sensor.
 2. The motion sensor of claim 1, wherein frequency of the clock signal is temperature compensated.
 3. The motion sensor of claim 1, wherein the digital circuit comprises an analog to digital converter (ADC).
 4. The motion sensor of claim 1, wherein the digital circuit comprises a low-pass filter.
 5. The motion sensor of claim 1, wherein the digital circuit comprises a motion processor; wherein the motion processor performs computation of algorithms for detection of movements or gestures.
 6. The motion sensor of claim 1, wherein the digital circuit comprises a memory.
 7. The motion sensor of claim 1, wherein the frequency translation circuit comprises a phase locked loop (PLL).
 8. The motion sensor of claim 1, wherein the digital signal comprises an interrupt signal.
 9. The motion sensor of claim 1, wherein the motion sensor comprises a gyroscope and the movement comprises angular velocity.
 10. The motion sensor of claim 1, wherein the movement comprises rotation.
 11. The motion sensor of claim 1, wherein the motion sensor comprises an accelerometer and the movement comprises acceleration.
 12. A vibratory gyroscope comprising: a MEMS structure that has a first and a second degrees of freedom, wherein the MEMS structure oscillates at a resonant frequency in the first degree of freedom and provides a sense signal in the second degree of freedom responsive to an angular velocity; a first electronic circuit coupled to the MEMS structure to detect motion of the MEMS structure in the first degree of freedom and to provide a drive signal; a second electronic circuit coupled to the MEMS structure to detect the sense signal; a frequency translation circuit coupled to the first electronic circuit, wherein the drive signal is translated to provide a clock signal; and a digital circuit coupled to the frequency translation circuit and the second electronic circuit, wherein the clock signal is utilized to drive the digital circuit and the digital circuit provides a digital signal that is related to the angular velocity.
 13. The vibratory gyroscope of claim 12, wherein the frequency of the clock signal is temperature compensated.
 14. The vibratory gyroscope of claim 12, wherein the digital circuit comprises an analog to digital converter (ADC).
 15. The vibratory gyroscope of claim 14, wherein the second electronic circuit further comprises: a sense amplifier coupled to the MEMS structure; and a demodulator coupled to the sense amplifier and to the ADC.
 16. The vibratory gyroscope of claim 12, wherein the digital circuit comprises a low-pass filter.
 17. The vibratory gyroscope of claim 12, wherein the digital circuit comprises motion processing; wherein motion processing performs computation of algorithms for detection of movements or gestures.
 18. The vibratory gyroscope of claim 12, wherein the digital circuit comprises a memory.
 19. The vibratory gyroscope of claim 12, wherein the frequency translation circuit comprises a phase locked loop (PLL).
 20. The vibratory gyroscope of claim 12, wherein the digital signal comprises an interrupt signal. 